Volume 36 Issue 10
Oct.  2021
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GUO Qiling, LIU Senyun, YI Xian, GUO Xiangdong, LIU Yu, YANG Shengke. Influence of sidewall interference in wind tunnel on rime ice on airfoil[J]. Journal of Aerospace Power, 2021, 36(10): 2197-2206. doi: 10.13224/j.cnki.jasp.20200517
Citation: GUO Qiling, LIU Senyun, YI Xian, GUO Xiangdong, LIU Yu, YANG Shengke. Influence of sidewall interference in wind tunnel on rime ice on airfoil[J]. Journal of Aerospace Power, 2021, 36(10): 2197-2206. doi: 10.13224/j.cnki.jasp.20200517

Influence of sidewall interference in wind tunnel on rime ice on airfoil

doi: 10.13224/j.cnki.jasp.20200517
  • Received Date: 2020-12-09
  • Publish Date: 2021-10-28
  • Numerical simulation was used to study the influence of sidewall interference on the process of ice accretion on NACA0012 airfoil under different blockage ratios.Research on the flow field and droplet trajectories showed that the sidewall can compress the air,causing more droplets to impact the leading edge of the wing,increasing the collection coefficient;the total amount of droplets collected on the wing surface was proportional to the blockage ratio and inversely proportional to the droplet Reynolds number;the sidewall can change the direction of droplet impaction,causing the offset of impingement limit and the position of the maximum local collection coefficient.The study of ice accretion using a multi-step method showed that the relative additional increment caused by the sidewall interference influence was about 16% under the baseline calculation condition,when the blockage ratio was 20% the relative additional increment icing mass in each time step was basically the same under the same blockage ratio.A factor reflecting the influence of sidewall interference on droplet collection was proposed,indicating an approximate linear relation with the additional increment of droplet collection.

     

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  • [1]
    易贤.飞机积冰的数值计算与积冰试验相似准则研究[D].四川 绵阳:中国空气动力研究与发展中心,2007.
    [2]
    ZOCCA M,GORI G,GUARDONE A.Blockage and three-dimensional effects in wind-tunnel testing of ice accretion over wings[J].Journal of Aircraft,2016,54(2):1-9.
    [3]
    杜雁霞,李明,桂业伟,等.飞机结冰热力学行为研究综述[J].航空学报,2017,38(2):25-36.
    [4]
    BARLOW J B,RAE W H,POPE A.Low-speed wind tunnel testing[M].3rd ed.Chichester,UK:John Wiley and Sons,1999.
    [5]
    钟世东,李巍,苏继川,等.三种跨声速洞壁干扰修正方法及其在小展弦比飞翼标模试验中的应用[J].空气动力学学报,2016,34(1):113-118.
    [6]
    刘光远,王瑞波,邓吉龙,等.基于涡流发生器的风洞侧壁附面层控制[J].航空动力学报,2016,31(9):2140-2145.
    [7]
    刘光远,魏志,彭鑫,等.跨声速风洞槽壁干扰评估与修正技术的应用[J].航空学报,2018,39(2):121499.1-121499.10.
    [8]
    江桂清.低速风洞常规试验的洞壁干扰修正方法[R].四川 绵阳:中国空气动力研究与发展中心,1983.
    [9]
    CASTRO B M,JONES K D,PLATZER M F,et al.Numerical investigation of transonic flutter and modeling of wind tunnel interference effects[J].Faculty and Researcher Publications,2003,23(1):1-9.
    [10]
    ALLAN M,BADCOCK K J.A CFD investigation of wind tunnel wall influences on pitching delta wings[J].Molecular Biology and Evolution,2002,22(11):1-8.
    [11]
    惠增宏,柳雯.风洞侧壁干扰控制与修正方法研究[J].实验流体力学,2010,24(6):73-76.
    [12]
    卢勇.自适应壁风洞原理应用于洞壁干扰修正的研究[D].西安:西北工业大学,2007.
    [13]
    GARNER H C,ROGERS E W E,ACUM W E A,et al.Subsonic wind tunnel wall corrections[R].Paris:Advisory Group for Aerospace Research and Development,1966.
    [14]
    焦予秦,王龙,高永卫,等.翼型极大迎角风洞试验技术研究[J].实验流体力学,2013,27(4):103-108.
    [15]
    李国强,张卫国,黄霞,等.翼型动态风洞试验洞壁效应研究[J].工程力学,2019,36(8):235-247.
    [16]
    QIN C,LOTH E.Numerical study of droplet trajectory and collection efficiency in IRT with large blockage effects[R].AIAA-2017-4376,2017.
    [17]
    CLARK C.Effects of wind tunnel aerodynamic blockage on stagnation collection efficiency in an icing environment[R].AIAA-2018-3832,2018.
    [18]
    BOURGAULT Y,HABASHI W G,DOMPIERRE J,et al.An eulerian approach to supercooled droplets impingement calculations[R].AIAA-97-0176,1997.
    [19]
    NILAMDEEN S,HABASHI W G,AUBé M S,et al.FENSAP-ICE:Modeling of water droplets and ice crystals[R].AIAA-2009-4128,2009.
    [20]
    FORTIN G,ILINCA A,LAFORTE,J L,et al.Prediction of 2D airfoil ice accretion by bisection method and by rivulets and beads modeling[R].AIAA-2003-1076,2003.
    [21]
    SHIN J,BOND T.Results of an icing test on a NACA 0012 airfoil in the NASA lewis icing research tunnel[R].AIAA-92-0647,1992.
    [22]
    杨胜华,林贵平.机翼结冰过程的数值模拟[J].航空动力学报,2011,26(2):323-330.
    [23]
    林贵平,卜雪琴,申晓斌,等.飞机结冰与防除冰技术[M].北京:北京航空航天大学出版社,2015.
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